Variable speed generator

ABSTRACT

A variable speed generator for producing AC electrical power includes an alternator to generate a first AC current, and a first rectifier which rectifies the first AC current from the alternator; a main exciter having a first field winding which receives the rectified first AC current and a first armature which produces a second AC current in response; a second rectifier which rectifies the second AC current from the first armature; a main generator having a second field winding which receives the rectified second AC current and a second armature which produces an output AC current in response; and a control arrangement for activating a selected pole configuration. The second field winding provides a plurality of selectively activatable pole configurations which differ in the number of their poles, such that the frequency of the output AC current can be varied by switching between the pole configurations.

The present invention relates to a variable speed generator forproducing AC electrical power, and particularly, but not exclusively, toan aircraft variable frequency starter generator.

With reference to FIG. 1, a ducted fan gas turbine engine generallyindicated at 10 has a principal and rotational axis X-X. The enginecomprises, in axial flow series, an air intake 11, a propulsive fan 12,an intermediate-pressure compressor 13, a high-pressure compressor 14,combustion equipment 15, a high-pressure turbine 16, andintermediate-pressure turbine 17, a low-pressure turbine 18 and a coreengine exhaust nozzle 19. A nacelle 21 generally surrounds the engine 10and defines the intake 11, a bypass duct 22 and a bypass exhaust nozzle23.

The gas turbine engine 10 works in a conventional manner so that airentering the intake 11 is accelerated by the fan 12 to produce two airflows: a first air flow A into the intermediate-pressure compressor 13and a second air flow B which passes through the bypass duct 22 toprovide propulsive thrust. The intermediate-pressure compressor 13compresses the air flow A directed into it before delivering that air tothe high pressure compressor 14 where further compression takes place.

The compressed air exhausted from the high-pressure compressor 14 isdirected into the combustion equipment 15 where it is mixed with fueland the mixture combusted. The resultant hot combustion products thenexpand through, and thereby drive the high, intermediate andlow-pressure turbines 16, 17, 18 before being exhausted through thenozzle 19 to provide additional propulsive thrust. The high,intermediate and low-pressure turbines respectively drive the high andintermediate-pressure compressors 14, 13 and the fan 12 by suitableinterconnecting shafts.

Electrical power is usually extracted from such an engine for use withinthe aircraft by a wound-field synchronous generator. The generator canbe mechanically connected to either the high-pressure shaft or to theintermediate-pressure shaft, via a transmission drive and accessorygearbox. DC current is applied to the rotor of the so generator in thefield winding. The frequency of the current produced in the generatorstator winding is thus directly proportional to the speed of the shaftto which the generator is connected, the gear ratio between the engineshaft and the generator, and the number of pole pairs in the generator.

In contemporary aircraft platforms, the output frequency range of thegenerator typically varies over a frequency range of 400 to 800 Hz; theexact numbers depending upon the platform, and corresponding directly toan acceptable speed range for the shaft to which the generator isconnected. The generator frequency range is provided to the suppliers ofelectrical equipment within the aircraft, so that their equipment can beconfigured to receive voltage in this frequency range.

Due to its variable output frequency, this type of generator is known asvariable frequency starter generator (VFSG). FIG. 2 shows a schematicdiagram of a VFSG, which includes a permanent magnet alternator (PMA)30, main exciter 31 and main generator 32. The rotating parts of thePMA, exciter and generator are physically all mounted on the same shaft33 and rotate at the same speed. The DC current injected into the fieldwinding of the main generator comes from a rotating diode rectifierwhich is powered from the main exciter, which in turn is powered fromthe PMA.

The PMA 30 has permanent magnets mounted on its rotor 34. As the rotorspins, an AC main exciter voltage is induced across the stationaryarmature winding 35 of the PMA. This winding is connected to a voltageregulator circuit 36 which rectifies a controlled amount of AC currentfrom the PMA stator winding and injects DC current into the stationaryfield winding 37 of the exciter 31. This in turn induces an AC voltageacross the rotating armature winding 38 of the exciter (the exciter isreferred to as inside out, with a stationary field winding and arotating armature winding). A rotating diode rectifier circuit 39,producing a DC current, is connected to the armature winding of theexciter. The output of this rotating rectifier is then connected to therotating field winding 40 of the main generator 32, inducing acontrolled, AC voltage across the generator's stationary armaturewinding 41. Due to the high speed of rotation of the shaft 33 inaerospace generators, a brushed system for applying field current to therotor of the main generator is not desirable.

The voltage regulator circuit 36 responds to changes in the load on thegenerator to maintain its output voltage at the required magnitude. Itdoes not affect the generator output frequency. In some arrangements,for example during starting, the PMA 30 may not be used and electricalpower can be provided directly to the exciter 31 from an alternativesource.

The use of a VFSG and direct mechanical coupling between the engineshaft and the generator means that a restriction on the frequency rangeof the generator electrical output maps directly to a speed rangerestriction on the engine shaft. The ratio of maximum to minimum speedis typically around 2.2:1 (producing a frequency range of e.g. 800 Hz to360 Hz).

If the VFSG and gearbox are configured to produce maximum frequency whenthe engine shaft is at its maximum speed, the minimum frequencycondition effectively imposes a minimum speed and therefore a minimumthrust condition on the engine. During idling conditions, such asdescent and taxiing, it is desired that the engine should produce aslittle thrust as possible, in order to save fuel. However, in order toremain within the electrical frequency range of the generator, the idlethrust of the engine may have to be set artificially high. Therefore itis desirable to have some degree of freedom between the electricalfrequency and the mechanical speed.

It would be desirable to provide a generator which can vary thefrequency of its output current independently of engine speed.

Accordingly, the present invention provides a variable speed generatorfor producing AC electrical power, the variable speed generatorincluding:

an alternator powerable by rotational action to generate a first ACcurrent,

a first rectifier which rectifies the first AC current from thealternator,

a main exciter having a first field winding which receives the rectifiedfirst AC current, and having a first armature which produces in responsea second AC current,

a second rectifier which rectifies the second AC current from the firstarmature, and

a main generator having a second field winding which receives therectified second AC current, and having a second armature which producesin response an output AC current;

wherein:

the second field winding is configured to provide a plurality ofselectively activatable pole configurations which differ in the numberof their poles, such that the frequency of the output AC current can bevaried by switching between the pole configurations, and

the variable speed generator further includes a control arrangement foractivating the selected pole configuration.

Advantageously, by switching between the pole configurations to vary thefrequency of the output AC current, the frequency can be changedindependently of the speed of the rotational action, such that theallowable rotational speed range can be increased. Furthermore, thevariable speed generator can be implemented without using brushes andslip rings.

The generator may have any one or, to the extent that they arecompatible, any combination of the following optional features.

Preferably, the pole configurations of the second armature arereconfigurable to match the number of poles in the second field winding,e.g. to make the number of poles on the second armature the same as thenumber of poles on the second field winding. For example, the controlarrangement can activate reconfiguration of the second armature at thesame time as activating the selected pole configuration of the secondfield winding.

Typically, the alternator has a rotor carrying one or more fieldmagnets, and a stator carrying an alternator armature in which the firstAC current is generated. Typically, the main exciter has a statorcarrying the first field winding, and a rotor carrying the firstarmature. Typically, the main generator has a rotor carrying the secondfield winding, and a stator carrying the second armature. Typically, themain exciter and main generator are powered by the same rotationalaction as the alternator. Conveniently, the rotors of the alternator,main exciter and main generator may be coaxially mounted in the variablespeed generator, and, in use, rotate at the same speed. For example,they may be mounted on the same rotatable shaft.

Preferably, the second rectifier is a diode rectifier. Such rectifiersare passive and generally reliable, particularly at the high rotationalspeeds which the rectifier may experience.

Preferably, the first rectifier is a voltage regulator circuit.

The second field winding may include a plurality of pole windings, theselectively activatable pole configurations being produced by switchingon or off and/or reversing the polarities of selected of the polewindings. For example, the control arrangement can include:

a control switch for changing the frequency of the distribution current,

a secondary exciter having a third field winding which on operation ofthe control switch receives the rectified first AC current, and a thirdarmature which produces in response a third AC current,

a third rectifier which rectifies the third AC current from the thirdarmature, and

a switching circuit which is activated by the rectified third AC currentto switch on or off and/or reverse the polarities of selected of thepole windings of the second field winding and thereby activates adifferent pole configuration. The switching circuit can then include aplurality of field effect transistors (e.g. MOSFETS), the rectifiedthird AC current providing gate currents for the transistors, and theconducting channels between the sources and drains of the transistorstransmitting the rectified second AC current from the second rectifierto the second field winding. For example, the polarity of each selectedpole winding may be changed by an arrangement of depletion mode andenhancement mode field effect transistors in the switching circuit. Inthis way, a reliable means of switching on or off and/or reversing thepolarities of selected of the pole windings can be achieved which canoperate at high rotational speeds and does not require the use ofbrushes and slip rings. Typically, the secondary exciter is powered bythe same rotational action as the alternator, main exciter and maingenerator. Typically, the secondary exciter has a stator carrying thethird field winding, and a rotor carrying the third armature.Conveniently, the rotor of the secondary exciter may be coaxiallymounted (e.g. on the same shaft) with the rotors of the alternator, mainexciter and main generator.

Alternatively, the second field winding may include first and secondindependently activatable winding formations, the first windingformation providing a pole configuration having a first number of poles,and the second winding formation providing a pole configuration having adifferent second number of poles, such that the frequency of the outputAC current can be varied by switching between the first and secondwinding formations. For example, the variable speed generator canfurther include:

a second main exciter having a third field winding which receives therectified first AC current, and having a third armature which producesin response a third AC current, and

a third rectifier which rectifies the third AC current from the thirdarmature;

wherein:

the first winding formation receives the rectified second AC current,

the second winding formation receives the rectified third AC current,and

the control arrangement can include a control switch which directs therectified first AC current to either the first field winding or thethird field winding to change the frequency of the distribution current.Typically, the second main exciter is powered by the same rotationalaction as the alternator, main exciter and main generator. Typically,the second main exciter has a stator carrying the third field winding,and a rotor carrying the third armature. Conveniently, the rotor of thesecond main exciter may be coaxially mounted (e.g. on the same shaft)with the rotors of the alternator, main exciter and main generator.

The variable speed generator can be a variable frequency startergenerator. More particularly, the variable speed generator can be anaircraft engine variable frequency starter generator, the alternatorbeing powerable by rotational action extracted from the aircraft engine,and the output current being for use within the aircraft.

Embodiments of the invention will now be described by way of examplewith reference to the accompanying drawings in which:

FIG. 1 shows a schematic longitudinal section through a ducted fan gasturbine engine;

FIG. 2 shows a schematic diagram of a variable frequency startergenerator;

FIG. 3 shows a schematic diagram of a variable frequency startergenerator according to a first embodiment of the present invention;

FIGS. 4( a) to (c) show respectively 8-pole, 4-pole and 4-pole salientpole configurations for the rotating field winding of the main generatorof the variable frequency starter generator of FIG. 3;

FIGS. 5( a) and (b) show respectively 8-pole and 4-pole configurationsfor the stationary armature winding of the main generator for use withthe pole configurations of FIG. 4;

FIGS. 6( a) and (b) show respectively 6-pole and 4-pole salient poleconfigurations for the rotating field winding of the main generator ofthe variable frequency starter generator of FIG. 3;

FIGS. 8( a) and (b) show respectively 6-pole and 4-pole configurationsfor the stationary armature winding of the main generator for use withthe pole configurations of FIG. 6 or 7;

FIG. 9 shows an arrangement of depletion mode (D) and enhancement (E)mode switches to switch the polarity of a pole winding; and

FIG. 10 shows a schematic diagram of a variable frequency startergenerator according to a second embodiment of the present invention.

FIG. 3 shows a schematic diagram of a VFSG according to a firstembodiment of the present invention. Like the VFSG of FIG. 2, the VFSGof the first embodiment includes a PMA 50, a main exciter 51 and a maingenerator 52. The rotating parts of the PMA, main exciter and maingenerator are all mounted on the same shaft 53 and rotate at the samespeed. The PMA has permanent magnets mounted on its rotor 54. As therotor spins, an AC main exciter voltage is induced across the stationaryarmature winding 55 of the PMA. This winding is connected to a voltageregulator circuit 56 which rectifies a controlled amount of AC currentfrom the PMA stator winding and injects DC current into the stationaryfield winding 57 of the main exciter. This in turn induces e.g. a 3phase AC voltage across the rotating armature winding 58 of the mainexciter. A rotating diode rectifier circuit 59, producing a DC current,is connected to the armature winding of the exciter. The output of thisrotating rectifier is then connected via a control arrangement(discussed below) to the rotating field winding 60 of the maingenerator, inducing an output AC voltage across the generator'sstationary armature winding 61. The field winding 60 is configured toprovide a plurality of selectively activatable pole configurations whichdiffer in the number of their poles, such that the frequency of theoutput AC current can be varied by switching between the poleconfigurations.

Unlike an induction machine, where the rotor poles are induced by thestator field, the rotating field winding 60 are directly supplied by theDC current from the rectifier circuit 59. However, the number of poleson the rotating field winding 60 can be varied without the use ofbrushes and slip rings, which would be undesirable due to the speed ofrotation of the shaft 53. More particularly, the field winding 60 hasindividual pole windings, and the number of poles on the field windingcan be varied by switching on or off selected of the pole windings, orreversing their polarities.

The rotating field winding 60 can be of round rotor design or salientpole design. FIG. 4( a) shows, for example, a salient 8-pole rotorconfiguration for the winding. Each saliency comprises an iron core anda pole winding, which produces a magnetic field when direct current isinjected into the pole winding. Depending on the polarity of theinjected current, the poles will be either North (N) or South (S)polarity. Typically, the poles will be arranged in alternatingpolarities to give an even distribution of flux.

Switching to a 4-pole configuration can be achieved by switching offhalf the pole windings and reversing the polarity on 2 of the remainingpoles, as shown in FIG. 4( b). To provide the same voltage on theterminals of the main generator 52, the amount of field current in therotating field winding 60 can be increased, increasing the flux densityin the iron cores of the active poles. The size of the poles isdetermined by the configuration with the lowest number of poles as themaximum allowable flux density is limited by the iron core material.

An alternative approach is to have all the poles active and to changethe polarity such that each magnetic pole is shared between 2 adjacentsaliencies, as shown in the configuration of FIG. 4( c). This allows theflux density to remain the same as the 8-pole configuration of FIG. 4(a), but may incur higher harmonic content than the configuration shownin FIG. 4( b).

The poles on the stationary armature winding 61 can be reconfigured byswitching armature winding connectors to match the number of poles onthe field winding 60. For example, FIGS. 5( a) and (b) show respectively8-pole and 4-pole configurations of the armature winding achieved byswitching the polarity of every second pole winding. In FIGS. 5( a) and(b), for convenience the armature is represented as a linear armatureand the pole windings are represented by single coils. The North (N) andSouth (S) poles are shown between the flux paths.

Depending on the specific application, it may be desirable to switch toa different ratio of poles, rather than the 2:1 ratio of FIGS. 4( a) to(c). For example, if switching from a 6-pole configuration to a 4-poleconfiguration, the rotating field winding 60 must contain the leastcommon multiple of saliencies i.e. 12. FIG. 6( a) shows a 6-poleconfiguration on such a 12 saliency pole rotor. To switch to a 4-poleconfiguration, four pole windings can be switched off, two pole windingscan be switched on, and the polarity of one pole winding can bereversed, as shown in FIG. 6( b). FIG. 7( a) shows an alternative 6-poleconfiguration on a 12 saliency pole rotor. To switch to a 4-poleconfiguration, the polarities of six pole winding can be reversed, asshown in FIG. 7( b). Advantageously, this configuration uses all theavailable saliencies to form the poles. FIGS. 8( a) and (b) showrespectively the corresponding 6-pole and 4-pole configurations of thestationary armature winding 61 achieved by placing, at the ends of thewindings, switches or contactors that connect different wires within thearmature together, to give the desired pole configuration.

Returning to FIG. 3, as mentioned above, the rotating diode rectifiercircuit 59, which produces a DC current, is connected via a controlarrangement to the rotating field winding 60 of the main generator 52.The control arrangement includes a secondary exciter 62, a passive (e.g.diode-based) rectifier circuit 65, and a rotating switching circuit 66,which are all located on the shaft 53 between the main exciter 51 andthe main generator. The secondary exciter is an inside-out machine,similar to the main exciter, in which the field winding 63 is located onthe stator and the armature winding 64 on the rotor. The secondaryexciter typically provides either single phase or 3-phase AC current onthe rotor, which is rectified to DC by the rectifier circuit 65. The DCcurrent is then fed to the switching circuit, which switches on or offand/or reverses the polarities, of selected of the pole windings of therotating field winding 60 to activate a different pole configuration inthe main generator 52.

The switching circuit 66 contains an arrangement of semiconductor-basedswitches. The conducting channels of the switches receive the output ofthe rotating rectifier 59. The secondary exciter 62 provides a gatecurrent to the switches. Each switch either switches on or offindividual pole windings of the field winding 60 or reverses thepolarity of the pole windings, to give a desired new pole configurationon the rotor of the main generator 52.

As the switches are typically required to carry approximately 10-100 A,they are generally high-powered devices such as power MOSFETs(metal-oxide-semiconductor field-effect transistors). Both depletionmode and enhancement mode MOSFETs can be used to switch from one poleconfiguration to another. The depletion mode MOSFETs conduct when thereis no gate current and open when gate current is applied, while theenhancement mode MOSFETs open when there is no gate current and conductwhen gate current is applied. For example, to switch the polarity of apole winding, an arrangement of depletion mode (D) and enhancement (E)mode switches can be used as shown in FIG. 9. In this arrangement thedepletion mode switches will conduct and the enhancement switches willopen when no gate current is applied, i.e. the secondary exciter 62 isnot providing power. When the secondary exciter is switched on itprovides gate current, opening the depletion mode switches and closingthe enhancement mode switches and thus reversing the polarity of thewinding.

This secondary exciter 62 generally has a lower rating than the mainexciter 51, as it only needs to provide gate current to the switches.

The control arrangement also includes a switch 67 which determineswhether or not the field current provided by the voltage regulatorcircuit 56 is sent to the secondary exciter 62. When the switch 67 isclosed, the secondary exciter 62 is activated and gate current flows tothe switches of the switching circuit 66. When the switch 67 is open,the secondary exciter 62 is disabled and no gate current flows. Theswitch 67 can also be operatively connected (dashed line) to thestationary armature winding 61 so that its poles are reconfigured tomatch the number of poles on the field winding 60 when the switch 67 isoperated.

The VFSG can switch poles on the main generator 52 during operation thusproviding a wider rotational speed range or the shaft 53 while remainingwithin a predetermined electrical frequency range of the output ACcurrent. The VFSG can provide and control its own reactive power andterminal voltage. As it does not require brushes and slip rings, it issuitable for high-speed applications and should not require high levelsof maintenance.

FIG. 10 shows a schematic diagram of a VFSG according to a secondembodiment of the present invention. Corresponding features have thesame reference numbers in FIGS. 3 and 10. Like the VFSG of the firstembodiment, the VFSG of the second embodiment includes a PMA 50, a mainexciter 51 and a main generator 152. However, an alternative arrangementused by the second embodiment for changing the poles on the rotor of themain generator 152 without the use of brushes and slip rings is to havea second main exciter 151 operating at the same power level as the firstmain exciter 51, along with a second rotating diode rectifier 159 forthe second main exciter. In addition, the rotating field winding 160 ofthe main generator 152 has first and second independently activatablewinding formations, each with a different number of poles. The outputsof the rotating rectifiers 59, 159 are then connected to respectivelythe first and second winding formations, inducing an output AC voltageacross the main generator's stationary armature winding 161. Forexample, first and second winding formations can be provided byrespectively a first set and a second set of pole windings on eachsaliency of the rotor of the main generator.

In the second embodiment, the control arrangement is simply a switch 167which switches the output of the voltage regulator circuit 56 from onemain exciter to the other. Again, the switch 167 can also be operativelyconnected to the stationary armature winding 161 so that its poles arereconfigured to match the number of poles on the field winding 160 whenthe switch 167 is operated.

However, a drawback of this the second embodiment is that it tends toincrease the overall size of the VFSG. Additionally, as there are twoseparate winding formations on the rotating field winding 160,undesirable voltage may be induced in the inactive formation.

Although the VFSG of the first and second embodiments is intended foraircraft use, a variable speed generator according to the presentinvention may also find use in other applications, particularly where itis desired to extend the rotational speed range of is the shaft and toavoid the use of brushes and slip rings.

While the invention has been described in conjunction with the exemplaryembodiments described above, many equivalent modifications andvariations will be apparent to those skilled in the art when given thisdisclosure. Accordingly, the exemplary embodiments of the invention setforth above are considered to be illustrative and not limiting. Variouschanges to the described embodiments may be made without departing fromthe spirit and scope of the invention.

1. A variable speed generator for producing AC electrical power, thevariable speed generator including: an alternator powerable byrotational action to generate a first AC current, a first rectifierwhich rectifies the first AC current from the alternator, a main exciterhaving a first field winding which receives the rectified first ACcurrent, and having a first armature which produces in response a secondAC current, a second rectifier which, rectifies the second AC currentfrom the first armature, and a main generator having a second fieldwinding which, receives the rectified second AC current, and having asecond armature which produces in response an output AC current;wherein: the second field winding is configured to provide a pluralityof selectively activatable pole configurations which differ in thenumber of their poles, such that the frequency of the output AC currentcan be varied by switching between the pole configurations, and thevariable speed generator further includes a control arrangement foractivating the selected pole configuration.
 2. A variable speedgenerator according to claim 1, wherein the second field windingincludes a plurality of pole windings, the selectively activatable poleconfigurations being produced by switching on or off and/or reversingthe polarities of selected of the pole windings.
 3. A variable speedgenerator according to claim 2, wherein the control arrangementincludes: a control switch for changing the frequency of thedistribution current, a secondary exciter having a third field windingwhich on operation of the control switch receives the rectified first ACcurrent, and a third armature which produces in response a third ACcurrent, a third rectifier which rectifies the third AC current from thethird armature, and a switching circuit which is activated by therectified third AC current to switch on or off and/or reverse thepolarities of selected of the pole windings of the second field windingand thereby activates a different pole configuration.
 4. A variablespeed generator according to claim 3, wherein the switching circuitincludes a plurality of field effect transistors, the rectified third ACcurrent providing gate currents for the transistors, and the conductingchannels between the sources and drains of the transistors transmittingthe rectified second AC current from the second rectifier to the secondfield winding.
 5. A variable speed generator according to claim 4,wherein the polarity of each selected pole winding is changed by anarrangement of depletion mode and enhancement mode field effecttransistors in the switching circuit.
 6. A variable speed generatoraccording to claim 1, wherein the second field winding includes firstand second independently activatable winding formations, the firstwinding formation providing a pole configuration having a first numberof poles, and the second winding formation providing a poleconfiguration having a different second number of poles, such that thefrequency of the output AC current can be varied by switching betweenthe first and second winding formations.
 7. A variable speed generatoraccording to claim 6, wherein the variable speed generator furtherincludes: a second main exciter having a third field winding whichreceives the rectified first AC current, and having a third armaturewhich produces in response a third AC current, and a third rectifierwhich rectifies the third AC current from the third armature; andwherein: the first winding formation receives the rectified second ACcurrent, the second winding formation receives the rectified third ACcurrent, and the control arrangement includes a control switch whichdirects the rectified first AC current to either the first field windingor the third field winding to change the frequency of the distributioncurrent.
 8. A variable speed generator according claim 1, which is anaircraft engine variable frequency starter generator, the alternatorbeing powerable by rotational action extracted from the aircraft engine,and the output current being for use within the aircraft.